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Damping structure and unmanned aerial vehicle

A technology of unmanned aerial vehicles and shock parts, which is applied in the field of unmanned aerial vehicles and can solve problems such as impact

Active Publication Date: 2018-10-19
GOERTEK INC
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

When the shock absorption effect in a certain direction is not good and needs to be adjusted, once a certain parameter (shape, size, hardness, etc.) is changed, the shock absorption effect in the three directions will change at the same time. At this time, the original shock absorption effect is sufficient. Good Direction Gets Bad

Method used

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  • Damping structure and unmanned aerial vehicle
  • Damping structure and unmanned aerial vehicle
  • Damping structure and unmanned aerial vehicle

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Embodiment Construction

[0036] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.

[0037]It should be noted that all directional indications (such as up, down, left, right, front, back...) in the embodiments of the present invention are only used to explain the relationship between the components in a certain posture (as shown in the accompanying drawings). Relative positional relationship, movement conditions, etc., if the specific posture changes, the directional indication will also change accordingly.

[0038] In addition, in th...

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PUM

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Abstract

The invention discloses a damping structure and an unmanned aerial vehicle. The damping structure comprises a base and three damping assemblies; each damping assembly comprises a moving part, a connecting part and a damping piece; according to each damping assembly, each moving part is arranged at the corresponding connecting part in a retractable mode; a releasing retracting space is formed between each moving part and the corresponding connecting part; each damping piece is arranged in the corresponding releasing retracting space and is connected with the corresponding connecting part and the corresponding moving part; in addition, a first connection part is fixedly connected with a second moving part, the second connecting part is fixedly connected with a third moving part, and a thirdconnecting part is fixedly connected with the base; and every two telescopic directions of the first, second and third moving parts are arranged in an included angle mode. According to the technical scheme, multidirectional independent damping is achieved, and therefore the damping effect of the damping structure is better.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a shock-absorbing structure and an unmanned aerial vehicle using the shock-absorbing structure. Background technique [0002] In recent years, the drone industry has developed rapidly, and drones are widely used in various fields such as photography, entertainment, inspection, and even agricultural production. Shock absorption has always been a very important topic in the field of drones. The existing UAV shock absorption, whether it is the shock absorption of the gimbal, the FPV module, or the IMU module, is basically based on the shock absorption of the shock-absorbing ball and the shock-absorbing foam. The flexibility and elasticity of the shock ball and shock-absorbing foam buffer the vibration shock transmitted by the motor, thereby filtering out high-frequency vibration. [0003] However, there is currently no damping structure capable of independently da...

Claims

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Application Information

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IPC IPC(8): B64D47/00B64D47/08F16F15/04
CPCB64D47/00B64D47/08F16F15/04
Inventor 李印波卜凡利王大伟徐顺义杨雪
Owner GOERTEK INC
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